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A bypass adapter and a rapid prototyping control method of an aeroengine based on the bypass adapter

An adapter and bypass technology, which is applied in the field of control system experimental research, can solve problems such as high cost, complex structure, and poor anti-interference ability, and achieve the effects of good real-time performance, long transmission distance, and strong anti-interference ability

Inactive Publication Date: 2011-09-14
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0005] The purpose of the present invention is to solve the problems of high cost, complex structure and poor anti-interference ability in the existing aero-engine rapid prototype control system, and provide a low-cost, high-efficiency, anti-interference, simple application bypass adapter and its aero-engine Rapid Prototyping Control Method

Method used

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  • A bypass adapter and a rapid prototyping control method of an aeroengine based on the bypass adapter
  • A bypass adapter and a rapid prototyping control method of an aeroengine based on the bypass adapter
  • A bypass adapter and a rapid prototyping control method of an aeroengine based on the bypass adapter

Examples

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Embodiment

[0030] Embodiment, the rapid prototype control of the miniature turbojet engine based on bypass type adapter

[0031] Such as Figure 7 As shown, the micro-turbojet engine control system controls the engine starter motor, ignition, gas valve, oil valve and oil pump according to the collected speed and exhaust temperature signals. The ignition, gas valve and oil valve signals are switch output, and the oil pump signal is analog output. By using a common PC and a bypass adapter, the micro turbojet engine control system can be quickly constructed, and the control laws can be studied on the PC.

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PUM

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Abstract

The invention discloses a bypass adapter and a rapid prototyping control method of an aeroengine based on the bypass adapter and the adapter comprises a DSP nucleus module, a signal driving module and a signal conditioning module. The rapid prototyping control method employs the bypass adapter and a general PC mechanism to form a rapid prototyping control system, wherein the PC controls as an engine control computer, and the bypass adapter realizes the communication with the engine control computer in a mode of high-speed serial communication, and, as a terminal device of an engine controller and in a bypass operation mode, realizes the conditioning and collection of sensor signals and controls the output and drive of the signals, with the data transmission of the adapter adopting a host / slave real-time logic. The bypass adapter and the rapid prototyping control method of the aeroengine are easy to use, and have strong anti-interference capability and strong real-time capability.

Description

technical field [0001] The invention is used in the experimental research of the control system of the aero-engine to meet the requirement of quickly establishing the prototype of the electronic control system of the aero-engine, and belongs to the technical field of aero-engine control. The rapid prototyping experiment of the aero-engine electronic control system needs to quickly build an environment for debugging the control law, condition and collect the sensor signal, and output the current signal to drive the actuator. Background technique [0002] In the development process of aero-engine electronic control system, the method of rapid prototype control system can save cost and greatly speed up the product progress. Rapid prototyping control refers to the rapid establishment of control objects and controller models in the early stages of product development, and multiple offline and online tests on the corresponding control models or control algorithms to verify the fea...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
Inventor 黄向华张天宏于兵唐周军刘冬冬
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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